user manual

TABLE 3.2-18
MISSION J-2
LM-II PROPELLANT LOADING UNCERTAINTIES
Vent Line Volume
Tank Volume
Pressure Measurement (+5 PSIA)
Temperature Measurement (+-I.5°F)
Measured Density
Weight Measurement
ILoading Tolerances
Total Loading Uncertainlty
Vent Line Volume
Tank Volume
Pressure Measurement (+-5 PSIA)
Temperature Measurement (i. 5 °F)
Measured Density
Weight Measurement
1Loading Tolerance
Total Loading Uncertainity
Loading Temperature
Ullage Calculation
Tank and Manifold Volume
Total
Amendment 114
9/15/71
LM-II APS PROPELLANT
Fuel (ib) Oxidizer (ib)
±0.2 +-0.3
±0.8 +-I.3
±0.5 ±0.8
+-1.7 ±4.3
±0.7 ±0.5
+-0.5 +-0.5
±0.5 +-0.5
±4.8 ±8.2
LM-II DPS PROPELLANT
±0.2 ±0.3
±3.62 ±5.96
+-1.70 ±2.77
+-6.49 ±15.76
±2.55 ±1.70
±0.5 ±0.5
±0.5 +-0.5
±15.6 +-27.5
LM-II RCS PROPELLANT
±0.6 ±1.8
±0.4 ±0.6
±0.8 ±1.4
+-1.8 ±3.8
IThese will be known quantities after loading is accomplished.
3.2-109
SNA-8-D-027(III)REV 3